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New Member
Gabriel
Join Date: Apr 2017
Posts: 1
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I am doing simple simulations with 2D airfoil NACA0012 in Fluent to determinate the Cd and the Cl. After generating the mesh (tetrahedral) and established the parameters (Spalart-Almaras model, ideal gas), I initialized the calculation, but each iteration is taking about 8 minutes to show!!!
How do I solve this? Obs: I am solving in parallel with 4 cores and double precision. |
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| airfoils, fluent, iterations |
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